science 32
TRANSCRIPT
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Design and control of a direct drive wind turbine equipped with
multilevel converters
Mohamed Abbes a, Jamel Belhadj a,b,*, Afef Ben Abdelghani Bennani a,c
a LSE-ENIT, P.O Box 37, Belvedere, 1002 Tunis, Tunisiab ESSTT, P.O. Box 56, Monfleury, 1008 Tunis, Tunisiac INSAT, P.O. Box 676, North Urban Centre, 1080 Tunis, Tunisia
a r t i c l e i n f o
Article history:
Received 10 September 2008
Accepted 18 October 2009
Available online 20 November 2009
Keywords:
Direct drive wind turbine
NPC
Multilevel converters
Phase locked loop
Voltage dips
G.C.R
a b s t r a c t
This paper concentrates on the design and control of a three-level grid side converter (GSC) for direct
drive high power wind turbines. The three-level, neutral point clamped (NPC) topology was investigated.
The proposed control scheme, based on vector current control, offers very satisfying performances
regarding to structure stability and grid connection requirements (GCR). In order to have an accurate
evaluation of grid voltage source, two grid synchronization methods are developed and their perfor-
mances are compared. The GSC performances are evaluated under both normal and grid fault conditions.
Simulation results show that stability is maintained during voltage dips and that the proposed direct
drive wind turbine satisfies completely GCR.
Ó 2009 Elsevier Ltd. All rights reserved.
1. Introduction
Wind power is one of the most attractive renewable energy
sources since it does not emit pollutant and many countries have
a high level of wind potential. As a consequence, wind turbine
generator systems are coming into wide use in electricity genera-
tion. Today, there are many wind turbine manufacturers worldwide
and different generator and power electronics configurations are
used. The most commonly used concepts are the fixed speed
squirrel-cage induction generator, the doubly fed induction
generator (DFIG) and the direct drive topology using a permanent
magnet synchronous generator (PMSG). For the latter concept, the
gearbox is removed and replaced by a multi-poles permanent
magnet synchronous generator. Gearbox removal saves the costs of
lubrication, maintenance, and installation [1]. In addition, the
direct drive structure can operate without any reactive power
consumption and its performances agree perfectly with grid
interconnection guidelines for wind power plants [2]. Up to now,
major technological developments in the wind turbine industry
focus on cost reduction and operational reliability. In addition to
these basic targets, the principal concern of manufacturers at
present is to increase wind turbine production capacity. However,
design of more powerful wind turbines often leads to high values of
the DC bus voltage. These values could exceed voltage blocking
capacities of currently available power devices, and particularly for
direct drive structure since this topology is based on full-sized
power converters. Even if high power semiconductors can be used
in some cases, these components are characterized by high
conduction and commutation losses. Therefore, utilization of
multilevel converters in large sized wind turbines seems to be very
interesting. As for all other applications, integration of multilevel
topologies withinwind turbines would also reduce output harmonic
distortion and consequentlyoutputfilter size,reduce dV/dt and then
improve the whole structure electromagnetic compatibility
characteristics.
In this paper, a three-level grid side converter design for a 2MW
direct drive wind turbine fully satisfying GCR is presented (Fig. 3). A
three-level NPC converter model and simulation is discussed in
section II. The general control scheme of the multilevel Grid Side
Converter is given in section III. This scheme should particularly
control the produced power at the point of common connection
and minimize DC bus voltage ripple. To achieve these perfor-
mances, control method uses an inner grid current controller
combined with an outer DC bus voltage controller based on
instantaneous active and reactive powers. Section _V deals with the
grid synchronization issue. Two methods are described and their
performances under distorted utility conditions are evaluated.* Corresponding author. ESSTT, Electrical (GE), BP 56, Bab Menera, Tunis 1008,
Tunisia. Tel.: þ216 98 560 665; fax: þ216 71 391 166.
E-mail address: [email protected] (J. Belhadj).
Contents lists available at ScienceDirect
Renewable Energy
j o u r n a l h o m e p a g e : w w w . e l s e v i e r . c o m / l o c a t e / r e n e n e
0960-1481/$ – see front matter Ó 2009 Elsevier Ltd. All rights reserved.
doi:10.1016/j.renene.2009.10.021
Renewable Energy 35 (2010) 936–945
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Section V focuses on the proposed structure behaviour under
voltage dips conditions: Performances are then evaluated taking
into account stability and compliance with GCR.
2. Three-level NPC inverter topology and modeling
Multilevel converters offer many advantages for high powerelectronics applications. In particular, they permit operation at
higher DC voltage using series connected power semiconductors.
Today, many topologies of multilevel converters are available.
The diode-clamped was one of the first developed [3]. It provides
more than two voltage levels by connecting the output voltage to
series connected DC bus capacitors. This is achieved by clamping
diodes. Fig. 1 depicts the three-level NPC inverter topology: Each
of the three legs can provide one additional output voltage level
to that of the classical two-level inverter. The neutral point
voltage, corresponding to one half of the DC bus voltage, is
available at the output of each phase when appropriate diodes
are clamped.
For phase «a» for example, Table 1 gives for each state S a, the
switching signals T a1, T a2 and the output voltage V ag . Current iadc1 isthe a-phase component to the junction current idc 1.
According to table I, output voltages V (a,b,c ) g can be expressed as:
V ag ¼Xi ¼ 2
i ¼ 1
T ai  V ci (1)
In the case of a three phase balanced load, expressions of phase
voltages are:0@V an
V bnV cn
1A ¼1
3Â
0@ 1 0 À1À1 1 00 À1 1
1AÂ
0@V abV bc V ca
1A (2)
0@V abV bc V ca
1A ¼0@ 1 À1 0
0 1 À1À1 0 1
1AÂ0@V ag
V bg V cg
1A (3)
Equations (2) and (3) give:
0@V anV bn
V cn
1A ¼ 13
Â0@ 2 À1 À1À1 2 À1À1 À1 2
1AÂ0@V ag V bg
V cg
1A (4)
Then, inverter phase to line voltages are related to the switching
signals by:
0@V an
V bnV cn
1A ¼1
3Â
0@ 2 À1 À1À1 2 À1À1 À1 2
1AÂ
0BBBBBBBB@
Pi ¼ 2
i ¼ 1
T ai  V ciPi ¼ 2
i ¼ 1
T bi  V ciPi ¼ 2
i ¼ 1
T ci  V ci
1CCCCCCCCA(5)
Moreover, neutral point current idc 1 expression can be written as
(Table 1):
idc 1 ¼ ðT a1 À T a2Þ Â ia þ ðT b1 À T b2Þ Â ib þ ðT c 1 À T c 2Þ Â ic
¼ ic 1 À ic 2 ð6Þ
Voltage ripples of the two DC bus capacitors are calculated as follows
(Herein, DC bus voltage is assumed constant and C 1 ¼ C 2 ¼ C ):
ic 1 ¼ C ÂdV c 1
dt ¼ C Â
dðU dc À V c 2Þ
dt ¼ ÀC Â
dV c 2
dt ¼ Àic 2 (7)
Then:
dV c 1
dt ¼
1
C Â
idc 1
2(8)
dV c 2
dt ¼ À1
C Â idc 1
2(9)
Simulation results, carried on with a sine triangle modulation, are
given in Fig. 2. The voltage balance between DC bus capacitors is
>
>
ic2
ic1
d0
d2
d1
g
cb
aidc1
idc2
+
- Udc
Vc2
Vc1
Ta1
T'a2
T'a1
Ta2
Tc1
T'c2
T'c1
Tc2Tb2
T'b1
T'b2
Tb1
a b c
ia ib ic
C1
C2
Fig. 1. Three-level NPC inverter topology.
Table 1
Three-level inverter states (phase a).
S a T a2 T a1 V ag iadc1
0 0 0 0 0
1 0 1 V c1 ia
2 1 1 V c1 þ V c2 0
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maintained (Fig. 2b). The simulation parameters are: U dc ¼ 3KV ,
C 1 ¼ C 2 ¼ 2.5 mF for the DC bus and R ¼ 10U, L ¼ 0.1H , for the load.
3. Control strategy of the three-level grid side converter
The main attention of this paper is the design and control of the
GSC, so the power chain was simplified by replacing the turbine
generator-rectifier group by an equivalent current source (Fig. 3).
The proposed control strategy aims to keep DC bus voltage constant
and impose PQ (active and reactive) powers injected to the grid.
Connection to the grid is achieved through an inductor filter and
a transformer. A PI-regulator was implemented to control DC bus
voltage. Output of this first controller is taken as the active power
reference at the point of common connexion. Reference grid
currents, i2d_ref and i2q_ref , are calculated through active and reactive
power references, and grid voltages V 2d, V 2q. Then, an appropriate
control loop for these grid currents is used to provide reference
voltages, V 1d_ref and V 1q_ref , for the three-level PWM-inverter.
3.1. Vector current controller
GSC is connected to the grid through an inductor filter and
a transformer (Fig. 4). This connection is described by equations
(10), and (11):
V 1ðt Þ ¼ r T 1$i1ðt Þ þ
lT 1 þL f
$
di1ðt Þ
dt þLm$
dði1ðt Þ À m$i2ðt ÞÞ
dt (10)
V 2ðt Þ ¼ Àr T 2$i2ðt Þ À lT 2$di2ðt Þ
dt þ e02ðt Þ (11)
with:
e02ðt Þ ¼ m$e01ðt Þ ¼ m$Lm$dði1ðt Þ À m
$i2ðt ÞÞ
dt
This gives:
V 1ðt Þ ¼ r T 1$i1ðt Þ þ L1$di1ðt Þ
dt À M $
dði2ðt ÞÞ
dt (12)
V 2ðt Þ ¼ Àr T 2$i2ðt Þ À L2$di2ðt Þ
dt þ M $
dði1ðt ÞÞ
dt (13)
With:
L2 ¼ m2$Lm þ lT 2: Secondary cyclic inductance, M ¼ m$Lm:
transformer mutual inductance, L1 ¼ lT 1 þ L f þ Lm(L f : filter induc-
tance). In the synchronous reference frame «dq» equations (12) and
(13) are written as:
0 0.005 0.01 0.015 0.02 0.025 0.03 0.035 0.04
-2
-1
1
2
0
1.45
1.50
1.55
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
1.45
1.50
1.55
Vc1
Vc2
0 0.005 0.01 0.015 0.02 0.025 0.03 0.035 0.04
-50
0
50
Time [s]
Time [s]
Time [s]
×103
×103
a
b
c
Fig. 2. a) a-phase line to neutral voltage (V). b) Capacitors voltages (V). c) Load Currents (A).
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V 1d ¼ r T 1$i1d þ L1$di1d
dt À L1uS $i1q À M $
di2d
dt þ M uS $i2q (14)
V 1q ¼ r T 1$i1q þ L1$di1q
dt þ L1uS $i1d À M $
di2q
dt À M uS $i2d (15)
V 2d ¼ Àr T 2$i2d À L2$di2d
dt þ L2uS $i2q þ M $
di1d
dt À M uS $i1q (16)
V 2q ¼ Àr T 2$i2q À L2$di2q
dt À L2uS $i2d þ M $
di1q
dt þ M uS $i1d (17)
Introducing (16) into (14) and (17) into (15), the control system is
expressed as:
V 1d;q ¼L1$r T 2
M $i2d;q þ
L1
M $
L2 À
M 2
L1
!$
di2d;q
dt þ
L1
M $V 2d;q
ÀL1
M $
L2 À
M 2
L1
!uS $i2q;d þ r T 1$i1d;q ð18Þ
Considering the termsecdand ecqdefined as:
ecd;q ¼L1
M $V 2d;q À
L1
M $
L2 À
M 2
L1
!uS $i2q;d þ r T 1$i1d;q (_),(__)
And assuming that:
V bd;q ¼L1$r T 2
M $i2d;q þ
L1
M $
L2 À
M 2
L1
!$
di2d;q
dt
The block diagram modeling the grid connection can be described
as illustrated in Fig. 5:
With: K ¼M
L1 Â r T 2and sS ¼
ðL2 À M 2
L1Þ
r T 2.
V1d_c V1q_c
3L_Inverter
V2a V2b V2c
C C P
L_filter IGBT
TR d i r G
I rec
V1a_ref
i1c
V1dq_ref
V2d
3
2
s
Pulse WidthModulation
i1bi1a
i1d i1q
3
2s
ecd ecq+ +
i2a i2
3
2
i2c
V2q
+-
PI
PI
+
-
LP
Udc
i2dq_ref
referencecurrent’s
generation
Q ref P ref
Udc_ref
PI
Pcond ref ic_ref
-+
-
Pred = Udc×Irec
+ +
+
i2d i2q
PLL
Fig. 3. Grid Side Converter structure and block scheme of control algorithm.
Fig. 4. Inverter connection to the grid. Fig. 5. Grid connection block diagram.
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The above diagram shows that control voltages V 1dand V 1q affect
both grid current components i2d and i2q. Therefore, d and q axes
need to be decoupled to achieve grid currents control. This will be
done by introducing two new control inputsV 1d_c andV 1q_c . Control
voltages V 1dandV 1qare then derived from these control inputs and
compensation terms ecd,qas shown in Fig. 6:
Hence, the grid connection model is simplified to the new
system depicted by Fig. 7:
In this way, axes «d» and «q» are decoupled. Grid currents
control is achieved simply by deriving PI-regulators gains for eachof the above independent first order transfer functions. This is
performed by placing the zero of the PI controller over the pole of
the system:
TF OL ¼K I  ð1 þ si  sÞ
sÂ
K
1 þ ss  s(19)
Consequently, system closed loop transfer function will be:
TF CL ¼i2d
i2d ref ¼
1
1 þ sc  s(20)
sc is the closed loop time constant. Its expression is given by:
s
c ¼
1
K Â K I (21)
3.2. Generation of grid current references
Reference currents, i2d,q_ref , are deduced through the point of
common connection voltages and power references as follows:
i2d ref ¼P ref $V 2d þ Q ref $V 2q
V 22d
þ V 22q
(22)
i2q ref ¼P ref $V 2q À Q ref $V 2d
V 22d
þ V 22q
(23)
3.3. DC bus voltage controller
The DC bus model for the back to back NPC converters is
described by Fig. 8:In Fig. 8, R1 and R2 stand for the capacitors leakage resistances.
Assuming thatR1 ¼ R2 ¼ R, and C 1 ¼ C 2 ¼ C , DC bus voltage ripple is
given by:
C dU dc
dt ¼ C
dV c 1
dt þ C
dV c 2
dt ¼ ic 1 þ ic 2 (24)
According to the model represented in Fig. 8, equations (25) and
(26) can be deduced:
I red À I ond ¼ ic 2 þ ir 2 (25)
ic 2 þ ir 2 ¼ ic 1 þ ir 1 þ idc 1 (26)
Introducing (25) and (26) into (24) the model is simplified to:
Fig. 6. Control voltages reconstruction.
Fig. 7. Decoupled control of grid current components.
Irec
ir1
R2
R1 C1
C2
ir2
ic1
ic2
Iond
Idc1
Ib
Fig. 8. Simplified diagram of the NPC back to back converters.
PI
Udc_ref
UdcUdc
ib_ref
+-
+_
1
2
dci
2
1
R
RCs
Fig. 9. DC bus control.
V2a
V2b
V2c
RF
V2α
V2β
32
2
( )SV
arctgV
β
βαα
θ
θ
=S
~
Fig. 10. ab filter algorithm block scheme.
+
V2d
-PI+
v2d_ref = 0 1
s
nω
Δ
ˆsθ
V2q
V2a
V2b
V2c
αβ
αβ
αβ
αβ
αβ
dq
3~
2
1
V
2Vn
2V
+
ω
Fig. 11. dq Phase Locked Loop synchronization method.
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C dU dc
dt ¼ 2ðI red À I ondÞ À ðir 2 þ ir 1Þ À idc 1 (27)
Thus, DC bus voltage is calculated as:
C dU dc
dt ¼ 2ðI red À I ondÞ À
V c 1
Rþ
V c 2
R
À idc 1 (28)
As U dc ¼ V c 1 þ V c 2, (28) gives:
C dU dc
dt þ
U dc
R¼ 2ðI rec À I invÞ À idc 1 (29)
Introducing PI-regulator, the DC bus voltage control loop is
described by Fig. 9 (With ib ¼ Irec ÀIinv). The neutral point current is
seen as a constant perturbation, so the zero of the PI controller is
placed over the system pole and the closed loop transfer function is
obtained (eq. 30).
TF CL ¼1
1
K I Â 2Rs þ 1
(30)
The DC bus voltage controller is the outer loop, whereas the two
current loops are the inner ones. These are designed to reachsettling times very quickly. On the other hand, the outer controller
aims are stability and optimal regulation, and therefore it is
designed to have a biggersettling time, at least 10 times bigger than
for the inner loops. So, the inner and the outer loops can be
considered independent, and therefore, the current transfer func-
tion is not considered when the DC bus controller is designed.
4. Wind turbine grid synchronization
In order to calculate and control the «PQ» power flow to the
electrical grid and avoid wind turbines tripping, the phase angle of
utility voltage must be accurately detected. Several grid synchroni-
zation methods are proposed in [4]. In this section two synchroni-
zation algorithms will be analysed: the filtering in the ab stationary
frame and the phase locked loop (PLL). The last one is implemented
in the dq synchronous rotating reference frame (called also dqPLL).
4.1. ab filter algorithm
The phase angle of the utility grid can be obtained by filtering
input voltage signals as depicted in Fig. 10. The two voltage
components obtained from three phase transformation are filtered
in order to avoid angle detection errors due to voltage harmonics.
However, filtering will introduce signal delay which is unaccept-
able for angle detection accuracy. Therefore a proper filter design
has to be made. A resonance filter is used to filter the ab voltages
(Resonance frequency is equal to the grid frequency). Then, grid
angle is obtained by using the arctg function.
4.2. dq Phase locked loop
PLL technique is based on the synchronism between the utility
voltage vector and the synchronous reference frame «dq» (Fig. 11).
After transformation of grid voltages to the ab frame, voltage
components are normalized to the magnitude of the grid voltage
vector
kV 2abk ¼ ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
V 22a þ V 22b
q .
Then, Park transformation is applied to the normalized
components to obtain dq voltages in the synchronous rotating
reference frame. The lock is realized by settling V 2d_ref to zero. A PI-
regulator is used to control error between V 2d and V 2d_ref . Thisregulator output is the grid angular frequency variationDus and it
is added to the nominal grid angular frequency un. The grid angle
estimation bqs is obtained by integrating this summation. This angle
detection method can be directly implemented. However, for
Fig. 12. dq reference frame and grid voltage vector synchronisation.
Fig. 13. Voltage dips classification [5].
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Time [s]
×10
0.2 0.21 0.22 0.23 0.24 0.25 0.26 0.27 0.28
-2
0
2 ] V [ e g a t l o v d i r G
0.2 0.21 0.22 0.23 0.24 0.25 0.26 0.27 0.28
0
2
4
6
] s / d a r [
0.2 0.21 0.22 0.23 0.24 0.25 0.26 0.27 0.28
0
2
4
6
] s / d a r [
a
b
c
Fig. 14. Behaviour of the synchronization algorithm in the case of 50% unbalanced voltage dip (Type C). (a) Grid voltages. (b) ab filter algorithm signal (c) dqPLL signal.
0.2 0.21 0.22 0.23 0.24 0.25 0.26 0.27 0.28
-2
0
2 ] V [ e g a t l o v d i r G
a
0.2 0.21 0.22 0.23 0.24 0.25 0.26 0.27 0.28
0
2
4
6
] s / d a r [
b
0.2 0.21 0.22 0.23 0.24 0.25 0.26 0.27 0.28
0
2
4
6
] s / d a r [
c
Time [s]
×10
estimated angle
grid angle
estimated angle
grid angle
Fig. 15. Synchronization algorithms behaviour during frequency variation ( f ¼
47Hz ). (a) Grid voltages. (b) ab filter algorithm signal. (c) dqPLL signal.
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deriving PI-regulator parameters, a linear model for this structure
needs to be developed.A linear model is developed as follows: After normalization, ab
grid voltage components expressions become:
V n2a ¼V 2a
kV 2abk¼
V 2a ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiV 22a þ V 2
2b
q ¼ cosðqsÞ (31)
V n2b ¼V 2b
kV 2abk¼
V 2b ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiV 22a þ V 2
2b
q ¼ sinðqsÞ (32)
With:qs the grid angle as depicted in Fig. 12.
Considering that
bqs ¼
bqdq þ
Q2
, Park transformation applied to
the normalized voltage components gives:
V 2d ¼ cos bqs ÀQ2V n2a þ sin bqs ÀQ2V n
2b
(33)
V 2q ¼ Àsin
bqs À
Q2
V n2a þ cos
bqs À
Q2
V n2b (34)
Introducing (31) and (32) into (33) and (34), expressions of grid
voltages in the synchronous reference frame dq are:
V 2d ¼ sin bqs
V n2a À cos
bqs
V n2b ¼ sin
bqs À qs
(35)
V 2q ¼ cos bqs
V n2a þ sin
bqs
V n2b ¼ cos
bqs À qs
(36)
Assuming that the difference
bqs À qs remains close to zero, voltage
direct component can be written as follows:
Time [s]
Order of Harmonic
0.26 0.27 0.28 0.29 0.3
-40
-20
20
40 ] A [ t n e r r u C d i
r G
0 20 40 60 80 100
0
20
40
e d u t i n g a M c i n o m r a H
THD = 1.2%
a
0 20 40 60 80 100
0
1
2
e d u t i n g a M c i n o m r a H
THD = 2.7%
Time [s]
Order of Harmonic
0.26 0.27 0.28 0.29 0.3
-2
0
2 ] V [ e g a t l o V d i r G
×103b
0
Fig. 16. Grid current and voltage spectrum analysis. a) Grid current b) Grid voltage.
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V 2dz bqs À qs (37)
Consequently, the linear model transfer function of the dqPLL
structure is given by:
H ðsÞ ¼ bqs
qs¼
K pS þ K I
s2 þ K pS þ K I (38)
4.3. Evaluation of the studied synchronization algorithms
In order to test angle estimation precision, several types of grid
voltage dips have to be considered. Voltage dips are defined as
a drop in voltage magnitude which is a consequence of short-circuit
fault on the grid. Fig. 13 gives six of the most common voltage sags
as defined by Bollen [5].
Simulation results presented below show synchronization
algorithms behaviour under a 50% unbalanced voltage dip, type C
(Fig 14) andin thecaseof grid frequency variation,a commonfaultin
the power system(Fig.15). Fig.14b shows that during type C voltage
dip, ab filter algorithm fails to provide correct angle estimation. The
100 Hz frequency negative sequence due to the unbalanced fault is
filtered by theresonance filter butdifferencein amplitudes of theab
Fig. 17. Proposed low voltage ride through requirement (E. ON Netz) [7].
Fig. 18. GSC response during type C voltage dip. a) DC bus capacitor voltages, b) DC bus voltage. c) Produced power PQ. d) Produced power PQ (different time scale).
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voltage components produces perturbation in synchronization
signal. In addition, for the frequency variation fault, a time lag is
introduced between the estimated angle and the grid phase angle.
This is a natural consequence of delay causedby the resonancefilter.
On the other hand, dqPLL algorithm is able totrack grid phase angle
in both fault cases (Figs. 14c and 15c). In consequence of these
results, dqPLL is selected to achieve GSC control.
5. Performances of the NPC-GSC under grid disturbance
5.1. Power quality
The system power quality is analysed in comparison with the
IEEE 519 standards [6]. These codes define harmonic distortion
limits for distributed power systems such as wind turbines, PV or
fuel cells systems. Spectrum analysis of grid currents and voltages
at the point of common connection has shown that the total
harmonic distortion (THD) is about 1.2% for current and 2.7% for
voltage. This is less than the 5% rate recommended by the IEEE
standards for both current and voltage. Thus, the produced power
complies with IEEE recommendations (Fig. 16).
5.2. Low voltage ride through (LVRT) capability of the wind turbinebased on NPC-GSC
In this section, the behaviourof the proposedNPC-GSC structure
under voltage dips is investigated. In this work, structure perfor-
mances are evaluated in comparison with the requirements of the
Germanic system operator E. ON Netz [7]. According to these
standards, wind turbines must withstand all types of voltage dips.
Dips magnitude is described based on a time diagram which
specifies voltage drop limits (Fig. 17).
The GSC model was subjected to several network disturbances
to analyse its performances. As an example, Fig.18 shows operation
when an unbalanced, type C, voltage dip occurs at the point of
common connection. At the fault beginning, voltage falls to 20% of
the grid nominal voltage then it starts to recover after a 150 mstime delay as depicted by Fig. 17. Fig. 18a shows DC bus capacitor
voltages, which are disturbed by the voltage dip. Nevertheless, they
come back to their rated value after the fault is cleared. Thus,
capacitor voltage balance is kept. Also, DC bus voltage ripple does
not exceed 5% of its rated value (Fig. 18b). This ripple decreases
gradually and it is eliminated after the end of voltage disturbance.
According to these results, it is concluded that the PWM-GSC
equipped with an NPC three-level converter keeps its stability and
can stay connected to the grid during the total period of the low
voltage fault.
6. Conclusion
In this paper, a three-level NPC Grid Side Converter for directdrive wind turbine was investigated. A general control scheme for
this GSC was defined and a-Phase Locked Loop algorithm is
developed to ensure its synchronization with grid voltage. The
designed dqPLL has overcome all test conditions and estimated
angle bqs tracks exactly the real grid angleqs. Transient operation of
the multilevel PWM-GSC under unbalanced voltage conditions is
analysed. The importance of ride through capability is increasing,
because the amount of wind power connected to the grid is in
constant growth. To test the robustness of the GSC control algo-
rithm during unbalanced voltage conditions, different voltage dips
were applied to this structure. Simulation results show that
stability is maintained during voltage dips and DC bus voltages
return totheir rated value after the end of the fault. This means that
generation is not lost because of temporary excursions of voltage.The Produced power has an acceptable quality since grid current
and voltage distortion is under standard harmonic limits. In
conclusion, this structure satisfies completely GCR and it provides
all advantages of multilevel converters to direct drive wind
turbines.
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M. Abbes et al. / Renewable Energy 35 (2010) 936–945 945